mike gamble boeing gravity research paper
DESCRIPTION
A study into the true nature of Gravity (Part 1)TRANSCRIPT
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BOEING is a trademark of Boeing Management Company.
Copyright © 2009 Boeing. All rights reserved.
STUDY of GRAVITYSpace Propulsion and
Energy Science International Forum
(BOE 021209-054)
MIKE GAMBLE2/26/09
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BOEING Release Memo
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SPESIF PITCH NOTES 2/26/09
Figure 1A) This is the Boeing memo allowing the “Public Domain” release of
this “Study of Gravity”. All Boeing documents have to be reviewed and
approved before they can be presented or published.
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STUDY OF GRAVITY
INTRODUCTION Hello, my name is Mike Gamble, I am an electronics engineer for The Boeing Co.
(Seattle). A week ago I had no idea that I would be here to present this study. Would like to thank the chair person of this conference for pulling the right strings. This presentation is from a different perspective more of a macroscopic overview. Enjoy the gravity presentation and let me know what you think about it.
HISTORYI started this “Study of Gravity” back in 2007 more as a curiosity than research.
Looking in textbooks all you find about gravity is the statement that it is an attraction
between two bodies and varies as the mass and separation. I thought there must be more to it, so I started collecting data about the earth. In engineering you start
with a ballpark number (WAG or SWAG) and work the problem from there. Being of
the electronics type I was trained to think in terms of waves, harmonics and frequencies. The “wow moment” in the research came when I realized that the harmonic waveshapes were aligning very close to that of the measured data. After
that things got real interesting!
Mike Gamble ([email protected])Mg09
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Steps in Understanding Gravity
• Document existing, known and relevant data
• Mathematical analysis of this data leading to a wave shape (field)
• Generation of this field• Phase reversal of field (lift)
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Figure 2) “Steps in Understanding Gravity” is an outline of the tasks taken and the order preformed in doing this study. It was done in two parts as the total package would be too much information to cram into a single presentation.
The “Study of Gravity” (part1) deals with the documentation and math models concluding with
a functioning accelerating force (gravity) equation. 1) Research and documentation of existing, known and relevant data about the functioning of
the earth system. This systems approach includes the data and analysis of all the major parts, not just of the surface acceleration commonly call “gravity”.
2) Mathematical analysis of all this data. Chose MatLab as the number crunching software tool as it includes all the regular math functions, trig functions, matrix operations and high
powered ones like curve fitting, imaginary number operations plus Fourier transforms. The goal was to generate a math model that accounted for the total system’s operation.
The “Study of Gravity” (part 2) deals with the generation of this wave shape and proposed applications.
3) Generation of this accelerating force (gravity) wave by using regular (EM) ElectroMagneticfield equations. This would correlate the accelerating Force field (F-field) to the Electric field
(E-field) and the Magnetic field (B-field) giving equation(s) that could be tested and used. Phase reversal and synchronization of this field should generate a usable lifting force.
4) Proposed applications using this lifting force combined with other current technologies could be applied to space drive engines.
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GRAVITY DOCUMENTATION
What is Known
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Figure 3) “Gravity Documentation” all of the research data for this study
was from public domain no Boeing information was used in this presentation
the “Study of Gravity”. Most of the space data (magnetosphere, geo-sync
orbit, radiation belts) is from the NASA website. The earth’s structure and
core data (mantle, crust, atmosphere, ionosphere) is from various geological
websites.
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PHYSICS: Gravity
X axis (equator)
Y axis (polar)
Re = 1 Earth Radius (surface)
= 3963 Miles
Gav = Gravity Average (radial)
= 32.174 ft/sec2 @ Re=1
Re = 1 (surface)
PLANET
Spherical FieldN
S
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Figure 4) “Physics: Gravity” from the textbook this is the standard classical
definition. Starting with the basic definition that gravity is a radial
acceleration with an average value of 32ft/sec2 decreasing as the distance
squared. It was first discovered by Newton, something about getting hit on
the head with an apple.
Main points:
1) The “Equator” direction is defined as the X-axis (+X = radial out)
2) The “Polar” direction is defined as the Y-axis (+Y = north)
3) The (Re) radius of the earth is 3963 miles
4) Average surface value (Re=1) is -32ft/sec2
5) Varies inversely as the distance (radius) squared
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VAN ALLEN RADIATION BELTS(Donut Shaped Rings)
OUTER BELT
INNER BELT
BWout
(Belt Width)BWin
Re
Rin
Rout
(Belt Center Radius)
N
S
Re = 3,963 miles
Rin = 5,860 milesBWin = 2,640 miles
Rout = 12,400 miles
BWout = 6,200 miles
15,500 miles
9,300 miles
4,540 miles
3,963 miles
7,180 miles
Y-AXIS
X-AXIS
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Figure 5) “Van Allen Radiation Belts” moving further out from the earth’s
surface is the Van Allen Radiation Belts. These belts are actually two
concentric donut shaped rings. Which have a crescent (half moon) shaped
cross section when viewed from the side, they are thickest around the
equator and taper off to zero at both the poles. The inner belt starts about
500miles above the equator and is about 2,600miles wide. While the outer
belt starts about 5,300miles above the equator and is 6,200miles wide.
Main points:
1) The radiation belts are two concentric donut shaped rings above the
equator
2) All radius measurements are from the center of the earth
3) The (BW) Belt Width and (R) Radius are both measured at the equator
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GEOSYNC ORBIT
Rgeo = 26,156 Miles (6.6Re)
Re = 3,963 Miles (1Re) GeoSync = 22,193 Miles (above surface)
|
1Re
|6.6Re
PLANET
Rgeo
GeoSync
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Figure 6) “GeoSync Orbit” moving further out from the radiation belts is the
place known as geosynchronous orbit (GeoSync for short). This place
22,000miles above the equator is where all the communications satellites
are “parked”. It has the unique feature that satellites at this distance
(radius) have an orbital speed that exactly matches the earths rotation so
they appear to remain stationary (in one place) with respect to any point on
the earth’s surface even though they are moving at speeds of thousands of
miles per hour.
Main points:
1) The (Rgeo) radius of geosync orbit is 26,000miles (6.6 Re)
2) The (Re) radius of the earth is 3963miles
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MAGNETOSPHERE
(Rmag) Radius 13 -14Re
Wake Extends 100Re
Leading Edge (bow)
Deformed 3-4Re
Velocity(cir) = 2*pi*93,000,000miles/365*24hr
= 66,700 miles/hr
1) That’s magnetoSPHERE with the accent on “sphere”
2) A circle (sphere) is a poor aerodynamic shape, though “aero”
might not be the right word.3) Wake and bow compression caused by high speed
passage through some type of (fluid) media.
Planet
93Mmiles
Sun
Earth
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Figure 7) “Magnetosphere” moving much further out from GeoSync orbit is
the outer edge of the earth’s magnetic shell or magnetosphere. It is
located about 52,000miles above the equator. The shell would be a
perfect sphere, if not for the fact the earth was traveling at high speed
through some type of (fluid) media. Like a boat going through the water
the earth has a bow wave and leaves a long wake behind it. However, a
boat has a ridged bow structure and the earth does not. Therefore, the
front edge of the earth’s spherical shell (magnetosphere) is compressed
from the impact of this media.
Main points:
1) The magnetosphere has an outer radius (Rmag) of about 52,000 to
56,000miles (13-14Re)
2) The earth is orbiting the sun at about 67,000miles/hr
3) A sphere is a poor aerodynamic shape, though “aero”(air) is not the
correct media
4) Front of magnetosphere is compressed 12,000 to 16,000miles (3-4Re)
5) Leaves a long wake of about 400,000miles (100Re)
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GRAVITY ANALYSIS
Number Crunching
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Figure 8) “Gravity Analysis” the number crunching section contains two
short tutorials and the main section on waveshape generation followed by a
short tutorial on Tesla’s work. The first tutorial is on the relevant
mathematical equations used in the analysis and the other on wave basics
as they apply to this study. The waveshape generation section shows what
forces are needed to construct the crescent shaped rings and spherical
shells along with their harmonic placements and frequencies.
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Relevant Equations
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Figure 9) “Relevant Equations” is a short tutorial on the mathematical
equations used in this study and how they apply to the math modeling.
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PHYSICS: Newton’s Law
F = M*A
EQUATION APPLIES:
1) Force is proportional to Acceleration (in the presence of Mass)
2) Mass in a Force field will (try to) Accelerate
Force equals Mass times Acceleration
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Figure 10) “Physics: Newton’s Law” straight from the textbooks states that
“Force equals Mass times Acceleration”. This equation applies to the
analysis in two ways. First, it shows that in the presence of Mass, Force is
proportional or equivalent to Acceleration; Mass being the constant of
proportionality. And second, if a Mass is placed in a Force field it will (try to)
Accelerate unless it can not move (blocked force).
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CALCULUS: Acc/Velocity/Position
A = dV/dt = d P/d tAcceleration equals the derivative of Velocity or the second derivative of Position
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Figure 11) “Calculus: Acc/Velocity/Position” basic calculus shows the
correlation between position (p), velocity (v) and acceleration (a). First,
Velocity (v) equals the derivative (dp/dt) of position (p). Second,
Acceleration (a) equals the derivative (dv/dt) of Velocity (v). Therefore,
Acceleration (a) equals the second derivative (d2p/dt2) of position (p).
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PHYSICS: Left Hand Motor Rule
F = E X BForce equals Electric [E] field “[vector] cross product” Magnetic [B] field
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Figure 12) “Physics: Left Hand Motor Rule” shows that the force turning a
motor armature is related to the flow of the electric (E) field times the
strength of the magnetic (B) field; all fields being orthogonal (90deg) to each
other. This is only an empirical equation showing the general relationship of
all the fields as it needs correct constants added to be exact.
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Wave Basics
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Figure 13) “Wave Basics” is a short tutorial on waves in general starting
with the basic definitions and common names. It is background material for
understanding the acceleration waves and their analysis.
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Waves in General
(anti-node)
+ amplitude(pk)
-amplitude(pk)
(anti-node)Wavelength (Lambda)
(node) (node)(node)
0
½ Lambda
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Figure 14) “Waves in General” shows one cycle of a basic wave and
describes and defines its makeup. Nodes are the zero crossings or
transition points of the wave. The peaks or anti-nodes are the maximum
and minimum wave values. The unit of length for one cycle of a wave is
called wavelength (λλλλ = Lambda).
Main points:
1) Wave nodes
2) Wave amplitude and peaks
3) Wavelength (λλλλ)
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Wave Amplitude
Gav = Average Gravity Therefore: Gpk = Gav / .637= 32.174 ft/sec2 @ Re=1 = 32.174 / .637
= 50.509 ft/sec2 / 5280 ft Gpk = Peak Gravity = .01 miles/sec2 @ Re=1
Zero (0%)
Peak (100%)
Average = 63.7% Peak
RMS = 70.7% Peak
(node) (node)
(anti-node)
½ Lambda
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Figure 15) “Wave Amplitude” defines the three ways of measuring a wave’s
amplitude and shows the correlation between them. First, is the maximum
or peak (pk) value defined as 100%. Second, is the (RMS) Root Mean
Squared value of 0.707pk defined as 70.7%. And third, the average or DC
value of 0.637pk defined as 63.7%. Using these standard values for
conversion, the average value of the acceleration of gravity (-32.174ft/sec2
@ Re=1) can be converted to its peak value (-0.01miles/sec2) for the
analysis. The units of “feet” were also converted to “miles” as the math
modeling was done in those units.
Main points:
1) Three types of wave amplitude measurement
2) Conversion of the acceleration of gravity to its peak value
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STANDING WAVES
Reflected (Traveling) Wave
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Incident (Traveling) Wave
Resultant (Standing)
Wave
Two waves of equal amplitude traveling in opposite directions
generate a standing wave of double amplitude
0
1
-1
0
1
-1
0
-2
-1
2
1
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Figure 16) “Standing Waves” shows how a standing wave is generated.
Waves are either traveling (moving) or standing (stationary). When a
transmitted wave called an “incident” wave is reflected back totally or
partially these two (incident/reflected) traveling waves each going in
opposite directions combine (mix) to produce a resultant wave that is
stationary and only varies in amplitude. This basic textbook definition holds
only if the phase and frequency of the wave was not changed much in the
reflection. Real world wave analysis must account for these changes as
they appear as distortion and polarization in the results.
Main points:
1) Two types of waves: traveling and standing
2) The standing wave has double (2x) the traveling wave’s amplitude
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POLARIZED (rectified) WAVE
2
0
-2
3
0
-1
0
-1
1
Fund
Result
Second
Harmonic
Fundamental plus second harmonic (half amplitude)
results in a nonsymmetrical (polarized) wave
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Figure 17) “Polarized (rectified) Wave” if the reflected waves amplitude is
halved and its frequency is doubled from that of the incident wave then the
resultant standing wave will be what is called polarized. This waveshape is
not symmetrical (same amplitude) above and below the zero point, it is
pushed off to one side or the other. Usually it is caused by some phase
shifting between the two traveling waves. However, it can be beneficial if
DC rectification is wanted.
Main points:
1) Caused by a change in a waves: amplitude, frequency and phase
2) Generates DC wave rectification
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Wave Shape Generation
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Figure 18) “Wave Shape Generation” This is the main section of the
presentation and gives the details about how the different shapes and
structures are constructed. Proceeding with the wave harmonics and
placements needed to build them.
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Wave Shape (field) Analysis[donut shaped ring]
1) Angles and amplitudes of (radial) Acceleration needed to generate
the wave shape (+Acc = outwards, -Acc = inwards)2) The 3D wave shape (donut) is generated by two (2) feedpoints
centered at the origin (0,0) ½ Lambda apart (dipole) on the Y-axis
X axis
Y axis
Node (null) Line
(Acc = 0)
Acc3 (+/-30 deg)
Acc1 (+/-45deg)
Acc2 = max (0 deg)+
-
Anti-Node
(-Acc = max negative)
Anti-Node (+Acc = max positive)
Acc = 0 (+/-90deg)
Feedpoints
(dipole)
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Figure 19) “Wave Shape (field) Analysis (donut shaped ring)” to generate a crescent
shaped donut ring field pattern requires an acceleration wave beat frequency from
two different sources (dipole feedpoints). To place the acceleration maximum on the X-axis (equator) requires the dipole to be located on the Y-axis (polar) as the
feedpoints are orthogonal (90deg) to the point of maximum field strength. A dipole
feedpoint spacing of half lambda (λ/2) is required at the proper frequency. Pattern size is determined by the wavelength (inverse of frequency). This placement
generates a circular field pattern with a crescent shaped cross section having a
maximum field on the X-axis tapering to zero (no field) on the Y-axis. The cross sectional area of this pattern has a node (zero point) in the middle of the field pattern
which is bounded by a plus (+Acc) maximum amplitude on the inner radius and a
negative (-Acc) maximum amplitude on the outer radius producing an “S” shaped pattern in the acceleration wave.
Main points:
1) A crescent shaped ring pattern can be generated by a dipole sourced field pattern
2) Dipole wavelength is λ/2 which centered at the origin (0,0) on the Y-axis3) Wavelength determines the pattern size
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Wave Shape (field) Analysis[Spherical shell]
Node (null) Line
(Acc = 0)
Anti-Node
(-Acc = max negative)
Anti-Node
(+Acc = max positive)
X axis
Y axis
Acc1 (-180 to 180deg)
feedpoint
1) Angles and amplitude of radial Acceleration needed to generate the wave shape (+Acc = outwards, -Acc = inwards)
2) The 3D wave shape (shell) is generated by one (1) feedpoint centered
at the origin (0,0)
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Figure 20) “Wave Shape (field) Analysis (spherical shell)” to generate a
spherical shell field pattern requires an acceleration wave from only one
source (feedpoint) located at its center (0, 0). Pattern size is determined by
the wavelength (inverse of frequency). This placement generates a circular
shell field pattern with equal maximums on both the X-axis and Y-axis. The
cross sectional area of this pattern has a node (zero point) in the middle of
the field pattern which is bounded by a plus (+Acc) maximum amplitude on
the inner radius and a negative (-Acc) maximum amplitude on the outer
radius producing an “S” shaped pattern in the acceleration wave.
Main points:
1) A spherical shell pattern can be generated by a single sourced field
pattern
2) Feedpoint is centered at the origin (0,0) on the Y-axis
3) Wavelength determines the pattern size
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Wavelengths (Lambda)
Lambda
Radius(R) = Lambda / 2*pi
Rgeo = Lambda
Rmag = 2*Lambda
R
PLANET
Rgeo RmagGeosync
Orbit
Edge of
Magnetosphere
(2x) LambdaLambda
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Figure 21) “Wavelengths (lambda)” shows the major harmonic spacing
between the earth’s center out to GeoSync orbit and further out to the edge
of the magnetosphere. Also, shown is the harmonic distance of the earth’s
circumference. All distances are measured in wavelengths (λ). The radius
(Rgeo) of geosync orbit is λ as is the outer circumference of the earth.
However, the radius (Rmag) of the magnetosphere edge is double that 2λ.
Main points:
1) Outer circumference of the earth is lambda (λ)
2) Radius of geosync orbit is lambda (λ)
3) Radius of the magnetosphere edge is 2 lambda (2λ)
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RADIUS ESTIMATESPlanet Structure
733Miles
733 Miles2160 Miles
OUTERCORE
MANTLEATMOSPHERE
SURFACE (Re)
CRUST
INNER CORE
IONOSPHERE
CRUST
0
air
3943 Miles
3963 Miles
4013 Miles
4194 Miles
Radius(R) = 4194Miles (minimum)Rair = 4013Miles (air)
Re = 3963Miles (surface)
R
Rair
Re Lambda
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Figure 21A) “Radius Estimates (planet structure)” is a more detailed view of
figure 21 showing just the earth harmonics. It show the earth’s
circumference wave (λ) completely enclosing the ionosphere and the rest of the planet’s structure. The radius (R) to the edge of the ionosphere extends
about 230miles above the surface while the radius (Rair) to the edge of the
atmosphere only extends about 50miles above the surface of the planet.
Main points:
1) Radius (R) of the ionosphere is 4194miles
2) Radius (Rair) of the atmosphere is 4013miles
3) Radius (Re) of the earths surface is 3963miles
4) All distances are measured from the earth’s center
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GRAVITY FREQUENCIES(ESTIMATES)
GeoSync (Rgeo)Freq = C / Lambda Lambda = 6.6*3963(miles)
= 186,284(miles/sec) / 26,156(miles)
= 7.12Hz
Earth Radius (Re)Freq = C / Lambda Lambda = 2*pi*4194(miles)
= 186,284(miles/sec) / 26,352(miles)
= 7.07Hz(max)
Using: Fundamental Frequency 7.1Hz
Second Harmonic 14.2Hz
Third Harmonic 21.3Hz
Fourth Harmonic 28.4Hz
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Figure 22) “Gravity Frequencies (estimates)” shows two different ways of
estimating the frequency of the acceleration (gravity) waves using the
classical equation (Freq = C / λ). Which states that Frequency is equal to
the speed of light (C) divided by the wavelength (λ). First method uses the GeoSync orbit wavelength distance (Rgeo) in the calculation giving an
answer of 7.12Hz. Second method used the earth’s radius (Re) in the
calculation giving an answer of 7.07Hz. Taking the mathematical average of
these two numbers and rounding the answer gives the initial estimate of
7.1Hz for the fundamental frequency. The second harmonic 14.2Hz is two
times (2x) the fundamental, the third harmonic 21.3Hz is three times (3x) the
fundamental and the fourth harmonic 28.4Hz is four times (4x) the
fundamental.
Main points:
1) Wavelength to frequency conversion equation (Freq = C / λ)2) Two different methods used to calculate the frequency
3) Acceleration (gravity) wave frequency estimates are: 7.1Hz, 14.2Hz,
21.3Hz, 28.4Hz
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RADIATION BELTS
OUTER BELT
INNERBELT
BWout
(Belt Width)BWin
Re
Rin
Rout
(Belt Center Radius)
N
S
¼ Lambda
½ Lambda
Rin = ¼ Lambda Rout = ½ LambdaMg07
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Figure 23) “ Radiation Belts” is the same data as figure 5 “Van Allen
Radiation Belts” only the distance measurements (miles) are converted to
harmonic wavelengths (λ). The distance from the center of the inner
radiation belt (Rin) to the center of the earth is λ/4. The distance from the
center of the outer radiation belt (Rout) to the center of the earth is λ/2. All measurements are taken on the X-axis (equator).
Main points:
1) Inner belt radius (Rin) is λ/4
2) Outer belt radius (Rout) is λ/2
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Planet Core Types
Solid
Acc is negative @ R=0
R
Hollow – Thin Crust
R
Acc is positive @ R=0
Hollow – Thick Crust
R
Acc is 0 @ R=0
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Figure 24) “Planet Core Types” shows the three possible types of planet
core data. Depending on what the value of the acceleration (gravity) wave
is at the center of the earth (R = 0) the structure would be a solid if the wave
had a negative value or it would be hollow with a thick crust if the wave was
zero or it would be hollow with a thin crust if the wave had a positive value.
The higher the value of positive acceleration the thinner the crust gets. We
are not talking pizzas here, we are talking solid rock! The pictures show the
acceleration wave patterns and the resulting structural shapes.
Main points:
1) Planet core structure depends on the acceleration waveshape at (R = 0)
2) Three possible types (solid, hollow-thick crust, hollow-thin crust)
EOT_RT_template.ppt | 53Copyright © 2009 Boeing. All rights reserved.
Proposed Y-Axis Data Plots
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Figure 25) “Proposed Y-axis Data Plots” the next step in the analysis process is to collect and put together all the previousindividual pieces of data that are relevant for the Y-axis (polar) waveshape analysis.
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Proposed (Radial) Wave Shape(s)
0 0.5 1 1.5 2 2.5 3 3.5 4
x 104
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02Y-Axis Initial Core Estimates (Acc vs Distance)
Dotted= Hollow Core(thin)
Solid= Hollow Core(thick)
Dashed= Solid Core
Distance (miles)
Accele
ration (
mile
s/s
ec2)
|< Lamda
+ 1Re
+ 2Re
+ 3Re
+ 4Re
+ 5Re
+ 6Re
+ 7Re
+ 8Re
+ 9Re
+10Re
*
Geo Sync=|< 26154.5miles
|<- surface
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Figure 26) “Proposed (radial) Wave Shapes” this plot shows what the
proposed Y-axis (polar) waveshape would be to generate the given field
patterns. The composite waveshape shows the three different core types at
(R = 0) and the earths surface acceleration value of -0.01miles/sec2 at (R =
Re). Also, shown is the “S” shaped wave pattern (shell) at GeoSync (R = λ) and another smaller “S” shaped wave pattern out at the magnetosphere
edge (R = 2λ) but due to MatLab plotting software’s scaling issue it is off
page at 50,000miles. Distances are shown in harmonic wavelengths (λ), earth radius (Re) and miles. Note there are three separate composite
waveshapes one generated for each core type all superimposed on this
plot.
Main points:
1) Displays waveshapes for all three core types
2) Displays earth’s surface marker
3) Displays GeoSync orbit marker
4) Three types of distance measurements
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FFT of Proposed Wave Shape(s)
0 5 10 15 20 25 30 35 400
0.5
1
1.5
2
2.5
3
3.5
4
4.5x 10
-5
Dotted(thin)= 6.37Hz 14.11Hz 21.85Hz +/-0.46Hz
Solid(thick)= 5.92Hz 13.20Hz 20.49Hz
Dashed(solid)= 5.46Hz 12.75Hz 20.03Hz
Y-Axis Estimate - Frequency Domain (FFT)
Rela
tive P
ow
er
Frequency (Hz)
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Figure 27) “FFT of Proposed Wave Shapes” gives the (FFT) Fast Fourier
Transform for the three different core types in the Y-axis (polar); the
composite waveshapes are displayed in the frequency domain. As can be
seen from the plots all three core waveshapes are composed of
approximately the same three harmonics (6Hz, 13Hz, 20Hz). The main
differences are in wave amplitude and phasing. Looking a little closer only
two of the waves (solid core, hollow – thick crust) are decreasing in
amplitude with increasing frequency. Note a Fourier transform is a
mathematical operation that outputs the harmonic frequency content of a
given input waveshape.
Main points:
1) Valid FFT waveshape no discontinuities
2) All three waveshapes are composed of the same three harmonics
3) Only the solid core and hollow core – thick crust waveshapes have
decreasing amplitude
EOT_RT_template.ppt | 59Copyright © 2009 Boeing. All rights reserved.
Proposed X-Axis Data Plots
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Figure 28) “Proposed X-axis Data Plots” the following plots collect and put
together all the previous individual pieces of data that are relevant for the X-
axis (equator) waveshape analysis.
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Proposed (Radial) Wave Shape(s)
0 0.5 1 1.5 2 2.5 3 3.5 4
x 104
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02X-Axis Initial Core Estimates (Acc vs Distance)
Dotted= Hollow Core(thin)
Solid= Hollow Core(thick)
Dashed= Solid Core
Distance (miles)
Accele
ration (
mile
s/s
ec2) *
< >Inner Belt
*
<--- --->Outer Belt
|< 1/4 Lamda
|< 1/2 Lamda
|< Lamda
+ 1Re
+ 2Re
+ 3Re
+ 4Re
+ 5Re
+ 6Re
+ 7Re
+ 8Re
+ 9Re
+10Re
*
Geo Sync=|< 26154.5miles
|<- surface
Mg07
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Figure 29) “Proposed (radial) Wave Shapes” plot shows what the proposed X-axis (equator) waveshape would be to generate the given field patterns. The composite
waveshape shows the three different core types at (R = 0) and the earths surface acceleration value of -0.01miles/sec2 at (R = Re). Also, shown is the “S” shaped
wave pattern (shell) at GeoSync (R = λ) and another smaller “S” shaped wave pattern out at the magnetosphere edge (R = 2λ) but due to MatLab plotting software’s scaling issue it is off page at 50,000miles. Plot is similar to Figure 26) for
the Y-axis data but with additional data included for the inner belt located at (R =
λ/4) and outer belt located at (R = λ/2). Distances are shown in harmonic
wavelengths (λ), earth radius (Re) and miles. Note there are three separate composite waveshapes one generated for each core type all superimposed on this plot.
Main points:
1) Displays waveshapes for all three core types2) Displays earth’s surface marker3) Displays Inner and Outer belt markers
4) Displays GeoSync orbit marker
5) Three types of distance measurements
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FFT of Proposed Wave Shape(s)
0 5 10 15 20 25 30 35 400
1
2
3
4
x 10-5
Dotted(thin)= 6.37Hz 14.11Hz 32.32Hz 36.88Hz +/-0.46Hz
Solid(thick)= 5.92Hz 13.20Hz 20.49Hz 27.77Hz
Dashed(solid)= 5.46Hz 12.75Hz 20.03Hz 25.95Hz
X-Axis Estimate - Frequency Domain (FFT)
Rela
tive P
ow
er
Frequency (Hz)Mg07
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Figure 30) “FFT of Proposed Wave Shapes” gives the (FFT) Fast Fourier
Transform for the three different core types in the X-axis (equator); the
composite waveshapes are displayed in the frequency domain. As can
be seen from the plots all three core waveshapes are composed of the
same three harmonics (6Hz, 13Hz, 20Hz) as the Y-axis data but with the
addition of a fourth higher harmonic. The main differences are in wave
amplitude and phasing. Looking a little closer the same two waves
(solid core, hollow – thick crust) are decreasing in amplitude with
increasing frequency.
Main points:
1) Valid FFT waveshape no discontinuities
2) All three waveshapes are composed of the four harmonics
3) The radiation belts add an additional harmonic to the three harmonics of
the Y-axis data
4) Only the solid core and hollow core – thick crust waveshapes are
decreasing in amplitude
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Fast Fourier Transform (FFT)Erratas
• Does not give phase or sign data • Gives only relative freq. components
• Freq. bin width resolution (quantization error)
• Freq. shifts due to harmonic(s) phasing
• Gives only relative freq. amplitudes• Harmonic(s) phase and attenuation
dependent
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Figure 31) “Fast Fourier Transform (FFT) errata’s” like many other things it
is not a perfect mathematical operation some data is lost in the process.
First, the transform assumes all the harmonic components have the same
phase therefore all phase data is lost. Second, the amplitude data is only
relative to the different harmonics so the absolute amplitude value is also
lost. However, even with these problems an FFT does a good job of
showing the waveshape’s sub-harmonic components.
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Proposed Wave Shape(s)FFT Analysis
• Y-axis wave shapes generated by THREE harmonics,X-axis wave shapes use FOUR harmonics
• Hollow Core(thin)• Hollow Core(thick)• Solid Core
• Frequencies are CLOSE to the estimated numbers
CORE TYPE
• est. solid thick thin• 7.1Hz (5.46, 5.92, 6.37Hz +/- .5Hz)• 14.2Hz (12.75, 13.66, 14.11Hz +/- .5Hz)• 21.3Hz (20.03, 20.94, 21.85Hz +/- .5Hz)• 28.4Hz (25.95, 27.77, 36.88Hz +/- .5Hz)
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Figure 32) “Proposed Wave Shapes FFT Analysis” this figure correlates
and summarizes all the proposed X-axis and Y-axis data. FFT analysis of
the Y-axis waveshape shows it can be generated by using a fundamental
frequency along with the second and third harmonics. Further data
reduction shows the X-axis waveshape is generated by the same three
harmonics with the additional fourth harmonic. The fourth harmonic mainly
appears to generate the crescent shaped inner and outer radiation belts.
The FFT of the generated frequencies is close to the original estimated
ones for all three core types. As the proposed numbers show good
correlation in the first round of analysis there is a high degree of confidence
in the original design assumptions.
Main points:
1) Y-axis waveshape generated by three harmonics
2) X-axis waveshape generated by four harmonics
3) Fourth harmonic generates the radiation belts
4) FFT generated frequencies close to the estimated ones
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Wave Shape GenerationGiven
Four frequencies: Four phases: First (fundamental) 7.1Hz 0 deg (sin)Second 14.2Hz 90 deg (cos)Third 21.3Hz 180 deg (-sin)Fourth 28.4Hz 270 deg (-cos)
EquationAcc = A*sin(7.1Hz) +B*sin(14.2Hz) +C*sin(21.3Hz) +D*sin(28.4Hz)
cos cos cos cos-sin -sin -sin -sin-cos -cos -cos -cos
[phase / freq] [phase / freq] [phase / freq] [phase / freq]
Yields 64 possible combinations [phase / freq]Hollow (thick crust) – five (5) combinations (Acc=0 @ R=0)Hollow (thin crust) – six (6) combinations (Acc=+ @ R=0)Solid – seven (7) combinations (Acc= - @ R=0) Random – other 46 combinations
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Figure 33) “Wave Shape Generation (given)” The next step of the analysis is to
construct a working equation that will produce or calculate the original proposed
waveshape. Based on all the reduced data this equation will have four harmonic frequency terms. The frequencies being a 7.1Hz fundamental , a 14.2Hz second
harmonic, a 21.3Hz third harmonic and a 28.4Hz fourth harmonic. As the FFT does not give wave amplitude or phase data these must be determined empirically by
comparing the calculated waveshape back to the proposed one. Assume the
equation to have the form: Acc = Amplitude*sin(freq+phase). The phasing would need testing in each of the four quadrants: 0deg, 90deg, 180deg and 270deg.
Therefore the solution (4x4) matrix would contain four frequencies and four phases
producing 64 possible frequency/phase terms. The conclusion after running all 64 possibilities is as follows: five (5) combinations produced a hollow core – thick
crust, six (6) combinations produced a hollow core – thin crust and seven (7)
combinations produced a solid core. The other 46 combinations all produced various random waveshapes.
Main points:1) Acceleration equation contains four frequency terms
2) Amplitude and phase empirically determined
3) Solution matrix contains 64 possibilities
EOT_RT_template.ppt | 71Copyright © 2009 Boeing. All rights reserved.
Calculated Y-Axis Data Plots
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Figure 34) “Calculated Y-axis Data Plots” the following plots compare the
calculated acceleration equations for the Y-axis back to the proposed ones,
with individual plots for each of the different core types.
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Hollow Core (thin) Data
0 0.5 1 1.5 2 2.5 3 3.5 4
x 104
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02Y-Axis Hollow Core(thin) Estimate and Calculated (Acc vs Distance)
Solid= EstimateDotted= CalculationAcc= -1.60e+001Sin(7.07Hz) -1.60e+001Sin(14.13Hz) +1.20e+001Cos(21.20Hz)
Distance (miles)
Accele
ration (
mile
s/s
ec2)
|< Lamda
+ 1Re
+ 2Re
+ 3Re
+ 4Re
+ 5Re
+ 6Re
+ 7Re
+ 8Re
+ 9Re
+10Re
*
Geo Sync=|< 26154.5miles
|<- surface
Mg07
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Figure 35) “Hollow Core (thin) Data” plots the best of the six (6) hollow
core – thin crust equations back with the proposed hollow core waveshape.
As can be seen from the plot the calculated value (dotted line) does not
have very good correlation with the estimated one (solid). The conclusion
being that the core is not hollow with a thin crust or in mathematical terms
the acceleration at the center (R = 0) is not positive.
Main points:
1) Planet core is not hollow core – thin crust
2) Acceleration at R = 0 is not positive
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Hollow Core (thick) Data
0 0.5 1 1.5 2 2.5 3 3.5 4
x 104
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02Y-Axis Hollow Core(thick) Estimate and Calculated (Acc vs Distance)
Solid= EstimateDotted= CalculationAcc= -2.00e+001Sin(7.07Hz) -2.00e+001Sin(14.13Hz) -8.00e+000Sin(21.20Hz)
Distance (miles)
Accele
ration (
mile
s/s
ec2)
|< Lamda
+ 1Re
+ 2Re
+ 3Re
+ 4Re
+ 5Re
+ 6Re
+ 7Re
+ 8Re
+ 9Re
+10Re
*
Geo Sync=|< 26154.5miles
|<- surface
Mg07
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Figure 36) “Hollow Core (thick) Data” plots the best of the five (5) hollow
core – thin crust equations back with the proposed hollow core waveshape.
As can be seen from the plot the calculated value (dotted line) has a very
good correlation with the estimated one (solid). There is also a good match
at the surface and GeoSync markers. The conclusion being that the core
might be hollow with a thin crust or in mathematical terms the acceleration
at the center (R = 0) is zero.
Main points:
1) Planet core might be hollow core – thick crust
2) Acceleration at R = 0 is zero
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Solid Core Data
0 0.5 1 1.5 2 2.5 3 3.5 4
x 104
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02Y-Axis Solid Core Estimate and Calculated (Acc vs Distance)
Solid= EstimateDotted= CalculationAcc= -2.00e+001Cos(7.07Hz) -2.00e+001Sin(14.13Hz) -2.00e+001Sin(21.20Hz)
Distance (miles)
Accele
ration (
mile
s/s
ec2)
|< Lamda
+ 1Re
+ 2Re
+ 3Re
+ 4Re
+ 5Re
+ 6Re
+ 7Re
+ 8Re
+ 9Re
+10Re
*
Geo Sync=|< 26154.5miles
|<- surface
Mg07
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Figure 37) “Solid Core Data” plots the best of the seven (7) solid core
equations back with the proposed solid core waveshape. As can be seen
from the plot the calculated value (dotted line) does not have very good
correlation with the estimated one (solid). The conclusion being that the
core is not solid or in mathematical terms the acceleration at the center (R
= 0) is not negative.
Main points:
1) Planet core is not solid
2) Acceleration at R = 0 is not negative
EOT_RT_template.ppt | 79Copyright © 2009 Boeing. All rights reserved.
Calculated X-Axis Data Plot
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Figure 38) “Calculated X-axis Data Plot” only has to check the hollow core
– thick crust equation in the X-axis as the other two equations hollow core –
thin crust and solid core did not correlate in the Y-axis.
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Hollow Core (thick) Data
0 0.5 1 1.5 2 2.5 3 3.5 4
x 104
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02X-Axis Hollow Core(thick) Estimate and Calculated (Acc vs Distance)
Solid= EstimateDotted= Calculation
Acc= -2.00e+001Sin(7.07Hz) -4.00e+001Sin(14.13Hz) -2.60e+001Sin(21.20Hz) -2.60e+001Sin(28.27Hz)
Distance (miles)
Accele
ration (
mile
s/s
ec2) *
< >Inner Belt
*
<--- --->Outer Belt
|< 1/4 Lamda
|< 1/2 Lamda
|< Lamda
+ 1Re
+ 2Re
+ 3Re
+ 4Re
+ 5Re
+ 6Re
+ 7Re
+ 8Re
+ 9Re
+10Re
*
Geo Sync=|< 26154.5miles
|<- surface
Mg07
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Figure 39) “Hollow Core (thick) Data” as can be seen from the plot the
calculated value (dotted line) also has very good correlation with the
estimated one (solid) in the X-axis. There is a good match at the surface,
outer belt and GeoSync markers though the inner belt marker is a little off.
This conclusion confirms the Y-axis data (figure 36) that the core is
possibly hollow with a thick crust or in mathematical terms the acceleration
at the center (R = 0) is zero.
Main points:
1) Confirms Y-axis plot data
2) Planet core possibly hollow with a thick crust
3) Acceleration at R = 0 is zero
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Analysis of Wave Shape(s)Proposed VS Calculated
• Wave shape(s) – time domain• Feedpoint for Proposed and Calculated is the origin (0,0)• Y-axis Hollow Core -Thick Crust data tracks the GeoSync and
Magnetosphere points the best • X-axis Hollow Core – Thick Crust data also tracks data
– Inner belt location is offset a few miles • Frequencies and Amplitudes – freq domain
• All frequency data shows FFT quantization error• All calculated frequencies close to estimated frequencies
• Conclusions• Wave shape will change some with a change in feedpoint
(dipole) location• Using: “Hollow Core - Thick Crust”
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Figure 40) “Analysis of Wave Shapes (proposed vs calculated)”
summarizes the results of all the time domain estimated vs calculated data
plots. Conclusion is that the hollow core – thick crust equations tracks both
the estimated X-axis and Y-axis the closest. In the frequency domain the
calculated frequencies are close to the proposed (estimated) numbers in
spite of the FFT quantization errors. Note all these plots were run with a
single feedpoint at the origin (0, 0). Waveshapes could possibly change
using dipole feedpoints.
Main points:
1) Both time and frequency domain data correlate
2) Confirms core type and acceleration value
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Feedpoint (dipole) Analysis
Hollow Core(thick) Acc Amplitude
• Frequency Harmonic X-Axis Y-Axis7.07Hz Fund 20.0 20.0
14.13Hz Second 40.0(2x) 20.0(1x)21.20Hz Third 26.0(1.3x) 8.0(.4x)28.27Hz Fourth 26.0(1.3x) 0.0
• A feedpoint dipole in the Y-Axis of Lambda/2 @ 4th Harmonic(28.27Hz) will zero out that harmonic and also reduce the other two harmonics in Y-Axis.
• Dipole length of Lambda/2 @ 28.27Hz (4th) = Lambda/8 @ 7.07Hz (Fundamental)
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Figure 41) “Feedpoint (dipole) Analysis” a closer examination of figures 36 and 39
shows that there are some differences in the constant terms for the Y-axis and X-axis equations. Comparing the two equations the 7.07Hz fundamental frequency has the same gain of 20, but the 14.13Hz second harmonic has double the gain in
the X-axis while the 28.27Hz fourth harmonic is completely missing in the Y-axis. To correlate or combine these differences in gains a double (dipole) feedpoint is
needed rather then a single feedpoint. Using a half wave dipole (λ/2) feedpoint centered at the origin (0, 0) positioned in the Y-axis will zero the fourth harmonic
term and also reduce the other two harmonics in the Y-axis. Converting the
28.27Hz fourth harmonic dipole (λ/2) wavelength back down to the 7.07Hz
fundamental frequency requires a division by 4 equaling a wavelength of λ/8.
Main points:
1) Change from single to dipole feedpoints
2) Dipole centered at the origin (0, 0) in Y-axis3) Fundamental frequency is same amplitude in X and Y axis4) Second harmonic is reduced amplitude in Y-axis
5) Third harmonic is reduced amplitude in Y-axis
6) Fourth harmonic is canceled in Y-axis
7) Dipole length is λ/8 at the 7.07Hz fundamental frequency Main points:
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X-Axis Dipole Plot
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Figure 42) “X-Axis Dipole Plot” shows the results of combining the dipole
feedpoints with the equations from figures 36 and 39 which are single
feedpoint ones. Only the end of the dipole which is labeled “A/B” can be
seen as it is located in the Y-axis (polar) however its effect is greatest in
the X-axis (equator). Also, it cleaned up the inner and outer radiation
belt curves much better than with a single feedpoint. The largest effect
of the dipole is on the core type which changed from hollow core – thick
crust to solid core (negative acceleration at R = 0). Plot scaling was
reduced to include the magnetosphere edge (R = 2λ).
Main points:
1) Dipole feedpoints
2) Same Inner and Outer belt markers
3) Same GeoSync marker
4) Surface gravity slightly less
5) Core type changed to solid
6) X-axis plot now includes magnetosphere
7) More background ripple
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Y-Axis Dipole Plot
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Figure 43) “Y-axis Dipole Plot” shows the same dipole results as figure 42
only in the Y-axis (polar). The λ/8 dipole feedpoints labeled A and B are clearly marked at the origin (0, 0). The equation constants are now the
same as the X-axis (equator) because the dipole arrangement corrected
the differences. The Y-axis core type remains a solid. Plot scaling was
reduced to include the magnetosphere edge (R = 2λ).
Main points:
1) Dipole feedpoints visible
2) Same GeoSync marker
3) Surface gravity slightly more
4) Y-axis core also a solid
5) Y-axis plot includes magnetosphere
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ELLIPTICAL PLANET SURFACE
X-Axis (equator)
(Poles)
Y-Axis
Planet surface is out of round (flattened at poles) because of unequal (dipole) X and Y axis accelerations
< 32FT/SEC2
32FT/SEC2
> 32FT/SEC2
Lambda/8 dipole
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Figure 44) “Elliptical Planet Surface” taking a closer look at figure 42
shows the X-axis acceleration value is a little less then the 32ft/sec2
surface marker. While figure 43 shows the Y-axis acceleration value is a
little greater then the 32ft/sec2 surface marker everything else being the
same. Conclusion the planet’s surface is slightly elliptical rather then a
perfect sphere. The λ/8 dipole arrangement places the feedpoints closer to the surface in the Y-axis which increases the acceleration value causing
the polar region to flatten.
Main points:
1) Greater Y-axis acceleration
2) Flattened polar region
3) Elliptical surface (not a sphere)
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WAVE HARMONICSPlanet Structure
733Miles
733 Miles2160 Miles
OUTERCORE
MANTLEATMOSPHERE
SURFACE (Re)
CRUST
INNER CORE
IONOSPHERE
CRUST
0
air
3943 Miles
3963 Miles
4013 Miles
4194 Miles
Radius(R) = 4194Miles (7.07Hz)
Rair = 4013Miles (7.39Hz)Re = 3963Miles (7.48Hz)
R
Rair
Re Lambda (7.07Hz)
[Fundamental]
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Second Harmonic
(14.13Hz)
Third Harmonic(21.20Hz)
Fourth Harmonic
(28.27Hz)
1049Miles1400Miles
2100Miles
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Figure 44A) “Wave Harmonics (planet structure)” is a more detailed view of the earth’s interior core. First, the crust material is solid and brittle. This brittleness is what earthquakes fracture making mountains and
valleys. It also conducts electricity as all the world’s power grids are “grounded” to it . Second, the mantle material is more plastic or pliable, viscous is the technical term. Its composition is mainly silicates with some
traces of iron, if you can think of a granite rock frame as being flexible! This is also the molten material (igneous rock) that volcano’s spew out as lava. The mantle is under both high pressure and high
temperature. Third, the core material is composed of mostly iron and some nickel, the outer region being in the liquid state. In spite of the high temperatures the acceleration spike generates enough pressure to
solidify the inner region making it a spherical iron center. As the core temperature is above the Curie point it can not maintain a magnetic field of its own but, being made of iron it will certainly be influenced by an
electromagnetic one. This is the same planet structure data in figure 21A only with the four acceleration wave harmonics (gravity) superimposed on it. As can be seen from the figure the fundamental harmonic
completely encloses the entire system including the ionosphere. Second, all the higher harmonics (second,
third and fourth) reside in the liquid outer core region. It is all these wave harmonics mixing in the middle of the liquid outer core that cause it to rotate (spin), works just like the motor armature it is. As the core’s rate
of rotation (revolutions/hour) is much higher than the earth’s rotation (revolutions/day) there is a friction line generated in the region of the outer core to mantle interface. It is this friction that causes the planets
internal heat. Because it pliable the mantle functions as the earths dynamic spin balancer. If the crust moves out of alignment it causes internal pressures to build up in the mantle correcting it. Also has a built
in safety valve, that when too much pressure builds up some volcano will pop (erupt) making a vent. When the heat generated equals the heat lost and spin power equals drag the system becomes stable.
Main points:1) Fundamental wave encloses entire structure
2) Higher harmonics reside in the outer core
3) Wave mixing causes heat and motion
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Corresponding X and Y 3D Dipole Gravity Plots
1) Space normal orientation
2) Rotated to show harmonic detail
3) FFT harmonic plot
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Figure 45) “Corresponding X and Y 3D Dipole Gravity Plots” the following
figures are the same dipole X and Y-axis equations only now they are
combined in 3D color plots.
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3D Dipole Plot (normal)
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Figure 46) “3D Dipole Plot (normal)” is the space normal view with the
dipole positioned vertical on the polar axis. It shows the spherical
acceleration (gravity) waves radiating out into space from the dipole along
with the earth surface and radius markers. Also visible is the big
acceleration spike generating the solid core. Just visible but difficult to see
because of plot scaling are the inner belt at 1.5Re and outer belt at 3Re.
Main points:
1) Earths gravity field pattern
2) Surface and radius markers
3) Core generation spike
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3D Dipole Plot (rotated)
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Figure 47) “3D Dipole plot (rotated)” is the same Dipole plot in figure 46
only rotated 90deg with the acceleration spike vertical. This is a MatLab
software requirement to be able to plot the additional contour map below it
(all wave data is the same). The contour map enhances some
acceleration wave details.
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FFT of 3D Dipole Plot
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Figure 48) “FFT of 3D Dipole Plot” shows the four acceleration (gravity)
wave harmonics in the frequency domain. This waveshape is very similar
to the estimated FFT for the proposed solid core waveshape in figure 30.
It has two high peaks at 7Hz and 14Hz and two small peaks at 21Hz and
28Hz all in descending order.
Main points:
1) Four harmonic frequencies
2) Wave amplitude in descending order
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TESLA MEASUREMENTS
Colorado Springs Experiments
(1899 – 1900)
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Figure 49) “Tesla Measurements” the following is short tutorial on Tesla’s
Colorado Springs experiments preformed back around the turn of the
century. They are relevant to this “Study of Gravity” as he measured the
electromagnetic frequency spectra of the earth.
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Tesla Measured Data
Electromagnetic frequency spectra of earth:7.8 Hz @ 0.12mW/Hz
14.1 Hz @ 0.10mW/Hz 20.0 Hz @ 0.06mW/Hz25.0 Hz @ 0.05mW/Hz
FFT Plot:Plot data (four freqs) using 180deg phase (-sin)
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Figure 50) “Tesla Measured Data” shows the four frequencies and power
levels he obtained from his electromagnetic experiments. The frequencies
that Tesla measured were a 7.8Hz fundamental, a 14.1Hz second
harmonic, a 20.0Hz third harmonic and a 25.0Hz fourth harmonic.
Main points:
1) Measurements made a 100 years ago
2) Tesla’s numbers still valid
3) Four electromagnetic frequencies
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Tesla Measured Data FFT
0 5 10 15 20 25 30 35 400
0.02
0.04
0.06
0.08
0.1
0.12
Data: 6.83Hz 13.66Hz 19.58Hz 25.50Hz +/-0.46Hz
Pwr= -1.238Sin(7.8Hz) -1.238Sin(14.1Hz) -0.867Sin(20.0Hz) -0.867Sin(25.0Hz)
Tesla Data - Frequency Domain (FFT)
Pow
er
(mW
/Hz)
Frequency (Hz)
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Figure 51) “Tesla Measured Data FFT” is the Fourier analysis plot in the
frequency domain using Tesla’s frequency data from the previous figure.
Note the similarities to the FFT of 3D dipole plot of figure 48. It has the
same two high peaks at 7Hz and 14Hz and two small peaks at 20Hz and
25Hz all in descending order. Also, it has a much smoother waveshape.
Main points
1) Four harmonic frequencies
2) Amplitude in descending order
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Schumann Resonance Data
Electromagnetic frequencies:7.83 Hz First Harmonic 14.1 Hz Second Harmonic 20.3 Hz Third Harmonic26.4 Hz Fourth Harmonic32.4 Hz Fifth Harmonic
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Figure 51A) “Schumann Resonance Data” is essentially the same data as
Tesla measured much earlier only with an additional fifth harmonic. Tesla’s
numbers disappeared for many years only to reappear in the late 1950s
under a different name. At the time I started this study I knew nothing
about “Schumann Resonance” only had Tesla’s data. He never got much
credit for any of his work (power grid, electric motors).
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GRAVITY CONCLUSIONS
What it is
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Figure 52) “Gravity conclusions” this is the wrap up of the “Study of
Gravity” (part1). The following figure summarizes the major points of this
study.
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Gravity
• Generated by long (low freq) standing waves of radial acceleration
• Composed of a fundamental and three harmonics• Fund: 7.07 Hz - Second: 14.14 Hz• Third: 21.21 Hz - Fourth: 28.28 Hz
• Y-Axis dipole feedpoint – Lambda/8 • Solid core (Acc = negative @ R=0)
• Dipole shifted Acc @ origin from 0 (hollow) to negative (solid)
• Solid means - not hollow (might be liquid)• Acceleration at surface not the same in X and Y axis
• Dipole flattened polar (Y) axis • First three (fund, second, third) harmonics generate the
outer magnetosphere (shell)• Fourth harmonic generates the radiation belts (donuts)• Frequency determines Scale Factor (SF) - Size
• Works for atoms (high Ghz)• Electromagnetic origin (Tesla data)
• Similar FFT plots Mg07
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Figure 53) “Gravity” compiles and lists all the data and information obtained from the research and number
crunching done in taking a detailed look into this subject. The gravitational system of earth is composed of an accelerating force generated by long (low frequency) standing waves which do far more than just make
the 32ft/sec2 surface acceleration commonly called gravity. These waves extend out some 60,000miles (2 wavelengths) into space generating the complete Magnetosphere, a stable GeoSynchronous orbit and both
the inner and outer Van Allen radiation belts. This waveshape is composed of four frequencies a fundamental and three higher harmonics. The numbers being 7.07Hz for the fundamental, 14.14Hz for the
second harmonic, 21.21Hz for the third harmonic and 28.28 for the fourth harmonic. Looking the other way towards the center of the earth the fundamental frequency determines the outer edge of the ionosphere
while the three higher harmonics reside in the planets outer core region. This wave mixing causes the internal heat, pressure, forces and rotation of the planet. These waves are sourced or concentrated at
dipole feedpoints located on the Y-axis centered about the origin (0, 0); dipole distance being λ/8 at the fundamental frequency. The dual feedpoints cause a number of modifications to the system. First, it changes the core type from hollow (thick crust) to solid. Solid meaning not a hollow structure could be
liquid or a combination of liquid and solids. Second, it causes a flattening of the polar region changing a round sphere to egg shaped or an ellipsis. Third, it generates the crescent shaped inner and outer
radiation belts. The first three harmonics primarily determine the planets structure, GeoSync orbit and the magnetosphere while the fourth harmonic contributes the two radiation belts.
In doing the data reduction and number crunching two other facts were uncovered that are not directly related to the gravity study but need to be documented as well. First, it appears that frequency
determines the size or scale factor of a structure. If this is true then atoms would have a similar type structure only much smaller in size (very high frequency – GHz). Second, the waves of accelerating force
seem to be of electromagnetic origin. They track or correlate with the earth’s electromagnetic waves discovered by Tesla and Schumann in both frequency and amplitude much too close not to be connected
to them. The analysis of this electromagnetic connection is the subject of the “Study of Gravity” (part2).